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Grumman X-29
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Grumman X-29

Grumman X-29
Description
Role Technology Demonstrator
Crew 1
First Flight December 14, 1984
Manufacturer Grumman Aerospace Corporation
Dimensions
Length 48 ft 1 in 14.7 m
Wingspan 27 ft 2 in 8.8 m
Height 14 ft 3 in 4.3 m
Weights
Empty lb kg
Loaded lb kg
Maximum takeoff 17,300 lb 7,700 kg
Powerplant
Engines 1x General Electric F404 turbofan
Thrust 16,000 lb 71.3 kN
Performance
Maximum speed 1,200mph 1,930km/h
Range miles km
Service ceiling 55,000 ft 16,800 m
Rate of climb ft/min m/min
Wing loading lb/ft² kg/m²
Thrust/Weight
Avionics
Avionics

The Grumman X-29 explored a number of new technologies, the most immediately obvious being the forward swept wings and canard control service. The inherent aerodynamic instability of this arrangement required the use of computerised fly-by-wire control, and advanced composite materials were needed to make the wing sufficiently rigid without being unacceptably heavy.

Two X-29As were built by Grumman Aerospace Corporation, and first flown in 1984. The test program of the two planes continued for over a decade, and on December 13, 1985 one of them became the first FSW aircraft to fly supersonically in level flight.

The X-29A demonstrated excellent control and maneuvering qualities at an angle of attack up to 45 degrees.

The wing configuration made the craft inherently unstable. It could fly only with the constant corrections (up to 40 per second) provided by the computerised flight control system. The system was made up of three redundant digital computers backed up by three redundant analog computers. It was estimated that a total failure of the system was as unlikely as a mechanical failure in a normal airplane.

The first craft built is now on display in the USAF Museum.

Also See

This article contains information that originally came from a NASA website. All NASA information is in the public domain, with the exception of the NASA logo, which may not be used without permission. See here for more information.

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